About: Saturn INT-21

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The Saturn INT-21 was a study for an American orbital launch vehicle of the 1970s. It was derived from the Saturn V rocket used for the Apollo program, using its first and second stages, but lacking the third stage. The guidance unit would be moved from the top of the third stage to the top of the second stage. The INT-21 was never flown.

Attributes	Values
rdf:type	Thing mean of transportation Rocket rocket yago:WikicatCancelledSpaceLaunchVehicles yago:Artifact100021939 yago:Conveyance103100490 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 book yago:Rocket104099429 yago:Vehicle104524313 yago:Whole100003553
rdfs:label	Saturn INT-21 (en) Saturn INT-21 (fr) Saturn INT-21 (it) Saturn INT-21 (pl) Saturno INT-21 (pt)
rdfs:comment	La fusée Saturn INT-21 était une étude pour un lanceur orbital américain des années 1970. Sa version dérivée de la fusée Saturn V est réalisée avec le surplus d’équipements du programme Apollo. D'autres variantes comme Saturn INT-20 et Saturn V-23(L) avaient été aussi proposées afin d'utiliser les 2 dernières Saturn V (qui n'ont jamais été lancées). Cette version gardait la case à équipements au sommet de l'OWS alors que Saturn INT-21 aurait modifié l'emplacement des cases à équipements au sommet du S-II afin de permettre à INT-21 de transporter des cargaisons ne se fondant pas sur le S-IVB. (fr) The Saturn INT-21 was a study for an American orbital launch vehicle of the 1970s. It was derived from the Saturn V rocket used for the Apollo program, using its first and second stages, but lacking the third stage. The guidance unit would be moved from the top of the third stage to the top of the second stage. The INT-21 was never flown. (en) Il Saturn INT-21 sarebbe stato un razzo lanciatore americano a due stadi derivato dal Saturn V, con il quale è comunemente confuso. La differenza sostanziale è che l'instrument unit (che sovrintendeva alla rotta del razzo) era piazzata in cima al secondo stadio del missile, anziché al terzo (il S-IVB) che completava il Saturn V "classico", per permettere di inserire in orbita un payload indipendentemente dalla presenza del terzo stadio. Sostanzialmente, il missile Saturn INT-21 non ha mai volato, ma un missile molto simile è stato comunque lanciato: esso portava la stazione spaziale Skylab. Effettuò soltanto un volo, il 14 maggio 1973, per portare appunto in orbita la stazione spaziale Skylab. L'instrument unit però era montata sullo Skylab anziché sul secondo stadio: di fatto, era un norm (it) Saturn INT-21 – odpowiednik rakiety Saturn V w wersji dwustopniowej (bez stopnia S-IVB, statku Apollo CSM i lądownika LM), a także ostatnia ciężka rakieta Saturn. Była specjalnie zaprojektowana na potrzeby programu , który zakładał rozwijanie technologii i zastosowań wykorzystanych w programie Apollo. Dla tej rakiety proponowano rozwiązanie, by instrumenty telemetryczne i kontrolne przenieść na stopień S-II, lecz uznano, że nie ma takiej konieczności, gdyż stacja Skylab była zbudowana ze stopnia S-IVB, stąd instrumenty kontrolne mogły się tam pomieścić. (pl) O Saturno INT-21 foi um estudo para a construção de um veículo de lançamento orbital estadunidense na década de 1970. Foi derivado do foguete Saturno V usado para o Programa Apollo, usando seus primeiros e segundos estágios, mas sem o terceiro estágio. A unidade de guiamento seriam movida a partir do topo do terceiro estágios para o início do segundo estágio. O INT-21 nunca foi concluído. (pt)
foaf:name	Saturn INT-21 (en)
name	Saturn INT-21 (en)
foaf:depiction
dcterms:subject	1973 in spaceflight Saturn (rocket family) Cancelled space launch vehicles
Wikipage page ID	5217933 (xsd:integer)
Wikipage revision ID	1122922830 (xsd:integer)
Link from a Wikipage to another Wikipage	Rocket Saturn I Saturn IB Saturn I SA-1 Saturn V Saturn V Instrument Unit Boeing Apollo Applications Program Orbit LH2 Comparison of orbital launch systems S-IC S-II S-IVB Apollo program Skylab Skylab B 1973 in spaceflight Launch vehicle Liquid oxygen Florida North American Aviation Saturn (rocket family) Cancelled space launch vehicles Kennedy Space Center Kennedy Space Center Launch Complex 39 RP-1 UTC LOX Low Earth orbit Rocketdyne Space station Project Apollo J-2 (rocket engine) F-1 (rocket engine)
Link from a Wikipage to an external page	https://web.archive.org/web/20090827133909/http:/centennialofflight.gov/essay/SPACEFLIGHT/skylab/SP23.htm https://web.archive.org/web/20161228090424/http:/astronautix.com/s/saturnint-21.html
sameAs	Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21 Saturn INT-21
sites	Kennedy Space Center Kennedy Space Center Launch Complex 39
dbp:wikiPageUsesTemplate	dbt:Expendable_launch_systems dbt:Cvt dbt:Refimprove dbt:Reflist dbt:Short_description dbt:Use_mdy_dates dbt:Infobox_rocket/stage dbt:Infobox_rocket/payload dbt:Infobox_rocket dbt:US_launch_systems dbt:Rocketry-stub dbt:Saturns
thumbnail	wiki-commons:Special:FilePath/Skylab_launch_on_Saturn_V.jpg?width=300
manufacturer	North American Aviation Boeing (en) (en)

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